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Question 1: In R&D, how do "Design for Manufacturability" (DFM) principles impact the development of aerospace systems, particularly in the early stages?

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Question 2: How do you ensure that a new aircraft design complies with both military and civilian regulations?

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Question 3: Which factor most influences the selection of materials for high-temperature aerospace components, such as turbine blades?

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Question 4: During the analysis of dynamic loads on aerospace systems, what is the key factor to measure?

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Question 5: How does "Aerodynamic Testing" contribute to R&D for new aerospace vehicles, and what are the key challenges associated with it?

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Question 6: In prototype development for aerospace systems, which of the following is the most critical factor when choosing materials?

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